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  • Proceedings of the 34th International Symposium on Shock Waves, Volume 1: Fundamentals: ISSW34, July 16–21 2023, Daegu, South Korea

    Proceedings of the 34th International Symposium on Shock Waves, Volume 1: Fundamentals by Myong, Rho Shin; Kim, Heuy Dong;

    ISSW34, July 16–21 2023, Daegu, South Korea

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    Hosszú leírás:

    "

    Shock waves are strong pressure waves resulting from irreversible processes in elastic media, including gases, liquids, or solids, generated by supersonic aircraft, explosions, or phenomena that cause rapid changes in pressure. The conference proceedings of the 34th International Symposium on Shock Waves (ISSW34), held in Daegu, Korea, in 2023, cover theoretical, experimental, and computational studies of these shock waves and associated phenomena, addressing both fundamental and applied aspects. They serve as the most up-to-date resource for physicists, chemists, engineers, and applied mathematicians involved in shock wave research.

    The three-volume set present the latest studies on diverse topics, including shock waves in gases, liquids, and solids, as well as in internal flows, detonation, supersonic and hypersonic flows, nozzle flows, and supersonic jet. It also explores emerging topics such as advanced shock tube design and application, recent development in diagnostics and flow visualization, shock waves in multiphase flows, and detonation engines.

    Volume 1 contains 52 articles covering the fundamentals of shock waves, including physical and chemical properties of shock waves, shock-vortex interaction, and numerical and experimental techniques.

    "

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    Tartalomjegyzék:

    Shock Wave Boundary Layer Interactions Over a Forward Facing Step at Mach 6.- Effects of Reynolds Number and Ramp Angle on Gortler Vortices over a Compression Ramp.- Large Eddy Simulation of the Control of the Inlet Buzz Phenomenon in a Supersonic Air Inlet.- On The Nature Of The Fishtail Shock Shock Interaction In The Transonic Flow Past A NACA0012 Profile.- Shock fitted Calculation Of Steady Mach Reflections In Overexpanded Nozzles Using Structured Grids.- Frequency Analysis of Heat-Transfer signals in Hypersonic Transitional and Turbulent Boundary Layers.- Fifth Order Bound-, Positivity, and Equilibrium Preserving Affine Invariant AWENO Scheme for Two Medium γ based Model of Stiffened Gas.- Investigation of shock-shock interaction in variable Mach number flow.- Dynamic Interactions Between an Oblique Shock and a Moving Cylinder.- Shock Tube Chemiluminescence and Spectroscopic CO Measurements of Norbornadiene.- Assessment of Axial Variations of Temperature and Enthalpy in a NASA Arc Jet using Laser Absorption of Atomic Oxygen and Nitrogen.- Global Instability of the Interaction Between an Oblique Shock and a Laminar Boundary Layer.- Analysis of High Enthalpy Shock Boundary Layer Interaction using a Shock Strength Dependent Turbulence Model.- Measurements of Disturbances Generated Over Hypersonic Boundary Layers with Shock Interactions.- Numerical Simulation of Supersonic Dusty Gas Flow
    Over a Cylinder in the Eulerian Lagrangian Framework.- Stability of Planar, Cylindrical and Spherical Steady Shocks.- Richtmyer Meshkov Instability Coupled with a Chemical Reaction.- Mach Evolution of the Cylinder Wake Flow Bifurcations.- Coexistence of Different Mechanisms in Shock Wave/Turbulent Boundary Layer Interactions.- Navier-Stokes Simulation of a Strong Shock Vortex Interaction.

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